BR112013023410A2 - dispositivo de travamento e nacela de motor turbojato compreendendo pelo menos uma carenagem movente - Google Patents

dispositivo de travamento e nacela de motor turbojato compreendendo pelo menos uma carenagem movente

Info

Publication number
BR112013023410A2
BR112013023410A2 BR112013023410A BR112013023410A BR112013023410A2 BR 112013023410 A2 BR112013023410 A2 BR 112013023410A2 BR 112013023410 A BR112013023410 A BR 112013023410A BR 112013023410 A BR112013023410 A BR 112013023410A BR 112013023410 A2 BR112013023410 A2 BR 112013023410A2
Authority
BR
Brazil
Prior art keywords
nacelle
locking device
turbojet engine
engine locking
fairing
Prior art date
Application number
BR112013023410A
Other languages
English (en)
Portuguese (pt)
Inventor
Fabrice Provost
Pascal Soulier
Original Assignee
Aircelle Sa
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Aircelle Sa filed Critical Aircelle Sa
Publication of BR112013023410A2 publication Critical patent/BR112013023410A2/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/06Attaching of nacelles, fairings or cowlings
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B41/00Locks with visible indication as to whether the lock is locked or unlocked
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B63/00Locks or fastenings with special structural characteristics
    • E05B63/14Arrangement of several locks or locks with several bolts, e.g. arranged one behind the other
    • E05B63/143Arrangement of several locks, e.g. in parallel or series, on one or more wings
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B53/00Operation or control of locks by mechanical transmissions, e.g. from a distance
    • E05B53/003Operation or control of locks by mechanical transmissions, e.g. from a distance flexible
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S292/00Closure fasteners
    • Y10S292/04Automatic release latches
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S292/00Closure fasteners
    • Y10S292/11Cover fasteners
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T292/00Closure fasteners
    • Y10T292/08Bolts
    • Y10T292/0911Hooked end

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structural Engineering (AREA)
  • Lock And Its Accessories (AREA)
  • Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
  • Indication Of The Valve Opening Or Closing Status (AREA)
BR112013023410A 2011-03-29 2012-03-21 dispositivo de travamento e nacela de motor turbojato compreendendo pelo menos uma carenagem movente BR112013023410A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1152562A FR2973421B1 (fr) 2011-03-29 2011-03-29 Dispositif de verrouillage a detection mecanique de fermeture et ouverture
PCT/FR2012/050586 WO2012131230A1 (fr) 2011-03-29 2012-03-21 Dispositif de verrouillage à détection mécanique de fermeture et ouverture

Publications (1)

Publication Number Publication Date
BR112013023410A2 true BR112013023410A2 (pt) 2016-12-13

Family

ID=45974439

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013023410A BR112013023410A2 (pt) 2011-03-29 2012-03-21 dispositivo de travamento e nacela de motor turbojato compreendendo pelo menos uma carenagem movente

Country Status (9)

Country Link
US (1) US9701413B2 (ru)
EP (1) EP2691587B1 (ru)
CN (1) CN103477007A (ru)
BR (1) BR112013023410A2 (ru)
CA (1) CA2828924C (ru)
ES (1) ES2758049T3 (ru)
FR (1) FR2973421B1 (ru)
RU (1) RU2013147722A (ru)
WO (1) WO2012131230A1 (ru)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10655364B2 (en) 2012-12-07 2020-05-19 Capitol Development, Llc Locking system with multiple latches
EP2829474B1 (en) * 2013-07-22 2018-11-21 Airbus Defence and Space SA Monitoring system for monitoring a two-part-cowl lock unit
CA2960880C (en) 2014-09-09 2023-03-14 Hartwell Corporation Clevis sensing lock
US10267060B2 (en) * 2016-12-21 2019-04-23 The Boeing Company Apparatuses and methods for cowl latch indication
US10814996B2 (en) 2017-10-17 2020-10-27 Rohr, Inc. Fan cowl tie rod assembly
EP3480115B1 (en) * 2017-11-03 2021-04-14 Airbus Defence and Space, S.A.U. System for monitoring the state of a hook-keeper unit
US11142326B2 (en) * 2018-07-27 2021-10-12 The Boeing Company Mechanism for indicating position of a latch mechanism for an aircraft nacelle
US11338931B2 (en) * 2018-11-20 2022-05-24 Rohr, Inc. High visibility panel latch
FR3088906A1 (fr) * 2018-11-22 2020-05-29 Airbus Operations Nacelle d’aéronef comportant un capot a deux vantaux articulés
US11773623B2 (en) 2020-05-05 2023-10-03 Rohr, Inc. Systems and methods for high visibility latch handle

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US986659A (en) * 1910-11-26 1911-03-14 Russel & Erwin Mfg Company Lock-indicator.
US1749649A (en) * 1928-03-07 1930-03-04 Yale & Towne Mfg Co Indicator for locks
US2638770A (en) * 1949-01-28 1953-05-19 Independent Lock Co Hotel lock
FR1058591A (fr) 1952-06-20 1954-03-17 Cosmetica Y Perfumeria Espanol Bouchon doseur perfectionné
US2939307A (en) * 1956-09-10 1960-06-07 Jr Earl M Trammell Protective device for latchconditioning elements
US3087749A (en) * 1959-07-20 1963-04-30 Capton Robert Auguste Locks, especially for pivoting leaf doors
US4179143A (en) * 1978-01-31 1979-12-18 Shy Min C Fixed latch lock
US4938508A (en) * 1989-02-10 1990-07-03 Thomas Peter C Gate latch
US5044678A (en) * 1990-07-25 1991-09-03 Lectron Products, Inc. Solenoid operated latch device with movable pole piece
WO1993024368A1 (en) * 1992-05-22 1993-12-09 Short Brothers Plc Closure default indicator
US5664811A (en) * 1995-04-12 1997-09-09 Lectron Products, Inc. Fuel filler door actuator assembly with integral kick-out spring
US5836638A (en) * 1996-12-09 1998-11-17 Illinois Tool Works Inc. Fuel door assembly
IT1289824B1 (it) * 1996-12-31 1998-10-16 Itw Fastex Italia Spa Gruppo bocchettone di rifornimento carburante, particolarmente per un veicolo a motore.
DE10023382A1 (de) * 2000-05-12 2001-11-15 Bayerische Motoren Werke Ag Tankklappen-Betätigungsvorrichtung
DE10137035A1 (de) * 2001-07-30 2003-02-20 Daimler Chrysler Ag Tankklappenanordnung für einen Kraftwagen
FR2832752B1 (fr) * 2001-11-27 2004-08-06 Airbus France Dispositif indicateur de defaut de fermeture d'au moins un mecanisme de verrouillage interpose entre deux elements
US7252311B2 (en) * 2003-09-17 2007-08-07 Hartwell Corporation Motor driven latch
US7552954B2 (en) * 2006-02-13 2009-06-30 The Boeing Company Storage bin latch assembly
FR2920170B1 (fr) * 2007-08-20 2009-09-18 Aircelle Sa Dispositif de verrouillage
FR2920174A1 (fr) * 2007-08-20 2009-02-27 Aircelle Sa Dispositif de liaison entre les deux demi-coquilles d'une nacelle de moteur d'aeronef, et nacelle equipee d'un tel dispositif
ES2359305B1 (es) * 2008-07-09 2012-03-23 Eads Construcciones Aeronauticas, S.A. Dispositivo para una unidad de propulsión de una aeronave.
FR2966488B1 (fr) * 2010-10-21 2012-10-26 Aircelle Sa Dispositif de verrouillage a detection mecanique de fermeture et ouverture

Also Published As

Publication number Publication date
FR2973421B1 (fr) 2013-04-05
ES2758049T3 (es) 2020-05-04
CA2828924A1 (fr) 2012-10-04
WO2012131230A1 (fr) 2012-10-04
FR2973421A1 (fr) 2012-10-05
US9701413B2 (en) 2017-07-11
EP2691587A1 (fr) 2014-02-05
CA2828924C (fr) 2019-05-07
EP2691587B1 (fr) 2019-10-16
CN103477007A (zh) 2013-12-25
RU2013147722A (ru) 2015-05-10
US20140030079A1 (en) 2014-01-30

Similar Documents

Publication Publication Date Title
BR112013023410A2 (pt) dispositivo de travamento e nacela de motor turbojato compreendendo pelo menos uma carenagem movente
BR112014008570A2 (pt) reversor de empuxo para uma nacela de um motor turbojato e nacela para uma aeronave turbojato
BR112014009939A2 (pt) dispositivo de reversão de empuxo para uma nacela de motor turbojato e nacela de um motor turbojato
EP3039266A4 (en) WITH A GAS TURBINE ENGINE BRAZED ARCHITECTURE WITH OIL RINSE
BR112014001679A2 (pt) cone de escape para motor turbojato de aeronave
BR112014028731A2 (pt) reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato.
BR112014017430A2 (pt) reversor de empuxo do tipo cascata para um motor turbojato de aeronaves e nacela oara um motor turbojato de aeronaves
SG11201403706WA (en) Low noise turbine for geared turbofan engine
BR112014002212A2 (pt) dispositivo reversor de empuxo de uma nacela e uma nacela de um motor turbo- ventilador
EP3004564A4 (en) TURBO FAN MOTOR WITH GENERATOR
BR112014004264A2 (pt) nacela e montagem traseira da mesma para motor turbojato
BR112013014444A2 (pt) nacela para um motor turbojato de fluxo secundário e aeronave incluindo uma asa e uma nacela
EP3071885A4 (en) MULTILINGER STRUCTURE OF A TURBINE ENGINE WITH INTERNAL COOLING ELEMENT (DE)
BR112014015552A8 (pt) estrutura de motor de turbina a gás composta e método para a produção de uma estrutura composta de componente de motor de turbina a gás
BR112014001529A2 (pt) nacela de motor turbojato compreendendo uma parte fixa e um meio reversor de empuxo
GB2503713B (en) Engine assembly with an Exhaust Driven Turbine
BR112015005181A2 (pt) dispositivo reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato.
BR112014010136A2 (pt) reversor de empuxo para uma nacela de motor turbojato de aeronave e nacela
IL244983A0 (en) Combined turbo-jet and turbo-propeller engine
BR112015012033A2 (pt) dispositivo de centralização, nacela para motor turbojato e conjunto de propulsão para aeronaves
BRPI0822127A8 (pt) nacela para motor turbojato e aeronave
BR112015001709A2 (pt) cascata de reversor de empuxo, reversor de empuxo e nacela de motor de aeronave
EP3049655A4 (en) REAR BEARING GAS TURBINE BEARING ARRANGEMENT
BR112014006998A2 (pt) conjunto de propulsão de aeronave compreendendo um motor turbojato
EP2989313A4 (en) GEAR TURBINE ENGINE HAVING O-PIPE AND PUSH INVERTER

Legal Events

Date Code Title Description
B08F Application fees: dismissal - article 86 of industrial property law

Free format text: REFERENTE A 5A ANUIDADE.

B08K Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87)